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- W2050840249 abstract "In this paper, a study was conducted regarding the stability of a binary airfoil under stochastic disturbances with feedback control. A new stochastic controller has been developed and investigated via Monte Carlo simulation. In order to design the new controller, the original system is transformed to the second-order moment one. Then the optimal control parameters can be obtained by searching for the effectual control parameters in the second-order moment system. Finally, the numerical simulations are included to visualize the good performances in flutter suppression." @default.
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- W2050840249 date "2013-09-01" @default.
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- W2050840249 title "A FEEDBACK CONTROL STRATEGY FOR AIRFOIL FLUTTER UNDER RANDOM EXCITATION" @default.
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- W2050840249 doi "https://doi.org/10.1142/s0219477513500132" @default.
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